Spinning Characteristics of the XN2Y-1 Airplane Obtained from the Spinning Balance and Compared with Results from the Spinning Tunnel and from Flight Tests (1937)
NASA Technical Reports Server (NTRS) · leaf 4
1/10-scale model of the XN2Y-1 airplane was tested given for parts of the model for the 17 flight attitudes. in the N. A. C. A. 5-foot vertical wind tunnel and the six An analysis of the data and a discussion of the results components of the forces and moments were measured. of the analysis with… … Figure 1.—Line diagram of spinning-balance force system. be tested for comparative purposes in these three ways. APPARATUS AND MODELS The flight tests are reported in references 1 and 2, the results from the free-spinning tunnel in reference 3, The tests were made in the N. A. C. A. 5-foot vertical…
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